Fokker F.14

__NOTOC__ Infobox Aircraft
name=Fokker F.14


caption=
type=Seven/Nine passenger transport monoplane
manufacturer=Atlantic Aircraft
designer=
first flight=1929
introduced=
retired=
status=
primary user=United States Army Air Corps
more users=
produced=
number built=
variants with their own articles=The Fokker F.14 was an American seven/nine passenger transport aircraft designed by Fokker and built by their Atlantic Aircraft factory in New Jersey.

Development

The F.14 was a typical Fokker designed single-engine transport but unusually it had a parasol-type high wing carried on struts above the fuselage. It had a fixed tailwheel landing gear. The pilot had a cockpit behind the passenger cabin.

Variants

;F.14:Civil production version with a 525hp (391kW) Wright R-1750-3 radial engine.;F.14A:Civilian aircraft with 575hp (429kW) Pratt & Whitney Hornet radial engine;Y1C-14:Designation for 20 Hornet-powered examples bought for the United States Army Air Corps in 1931, later became the C-14.;Y1C-14A:Last of the 20 Y1C-14s re-engined with a 575hp (429kW) Wright R-1820-7 Cyclone.;Y1C-14B:Re-engined with a 525hp (391kW) Pratt & Whitney Hornet R-1690-5 Hornet engine.;Y1C-15:Conversion of the ninth Y1C-14 as an air ambulance.;Y1C-15A:Y1C-15 re-engined with a 575hp (429kW) Wright R-1820 Cyclone, later C-15A.

Operators

;USA
*United States Army Air Corps

pecifications (F.14)

aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1878
met or eng?= eng

crew=1
capacity=seven/nine passengers
length m=13.18
length ft=43
length in=3
span m=18.11
span ft=59
span in=5
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=3.76
height ft=12
height in=4
wing area sqm=51.19
wing area sqft=551
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1971
empty weight lb=4346
gross weight kg=3266
gross weight lb=7200
lift kg=
lift lb=

eng1 number=1
eng1 type=Wright R-1750-3 9-cylinder radial
eng1 kw= 391
eng1 hp= 525
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
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max speed kmh=220
max speed mph=137
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=110
range miles=690
endurance h=
endurance min=
ceiling m=4420
ceiling ft=14,500
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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aircontent
see also=
related=
similar aircraft=
sequence=
lists=
*List of military aircraft of the United States

References

* John Andrade, U.S.Military Aircraft Designations and Serials since 1909, Midland Counties Publications, 1979, ISBN 0 904597 22 9 (Page 62)
* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1878.